1.
The pressurization system is capable of
maintaining a cabin altitude of 8,000 feet
at a maximum cabin differential pressure
when the airplane’s actual altitude is:
A. 31,000 feet
B. 41,000 feet
C. 43,000 feet
D. 35,000 feet
2.
The pressurization system can maintain a
maximum cabin differential pressure of:
A. 7.35 psi
B. 8.55 psi
C. 9.35 psi
D. 5.38 psi
3.
The maximum allowable negative cabin
differential pressure is:
A. 0.5 psi
B. 8.55 psi
C. 1.25 psi
D. 0.025 psi
4.
With the airplane on the ground and the
air-conditioning system on, the PRESSN
switch prevents cabin pressurization when
in the:
A. OVRD position
B. ON position
C. OFF position
D. AUTO position
5.
If the pressurization system fails, exces-
sive cabin pressure is prevented by the:
A. Outflow/safety valve
B. Dump valve
C. Pressure controller
D. Ram-air valve
12-9
FOR TRAINING PURPOSES ONLY
HAWKER 800 XP
PILOT TRAINING MANUAL
FlightSafety
international
QUESTIONS
Summary of Contents for 800 XP
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